Optimization of peened-surface laser shock conditions by method of finite element and technique of design of experiments
This paper presents a numerical simulation of the laser shock peening (LSP) process using the finite element method. The majority of controlling parameters of the LSP process have been taken into account. The LSP loading has been characterized by the use of a repetitive time Gaussian increment press...
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Published in | International journal of advanced manufacturing technology Vol. 97; no. 1-4; pp. 51 - 69 |
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Main Authors | , , , , |
Format | Journal Article |
Language | English |
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Springer London
01.07.2018
Springer Nature B.V |
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Abstract | This paper presents a numerical simulation of the laser shock peening (LSP) process using the finite element method. The majority of controlling parameters of the LSP process have been taken into account. The LSP loading has been characterized by the use of a repetitive time Gaussian increment pressure applied uniformly at a circular impacted zone. The utilized model of the treated material behaviour law is the Johnson-Cook’s visco-elastic-plastic coupled with damage. The proposed model leads to determine the LSP surface modifications: (i) the in-depth residual stresses, (ii) the induced plastic strains and (iii) the superficial damage. These modifications can be significantly induced in few cases, particularly when the operating conditions are not well optimized. An application is carried out on the laser peened titanium aero-engine super alloy Ti-6Al-4V. A satisfactory correlation between the computed and experimental results is observed. Also, it is noted that the computed superficial damage values increase with the growth of the maximal peak pressure of the laser spot, which are physically consistent. Otherwise, in order to optimize the laser peening operating conditions, a design of experiments is established. It allows having surface-response relationships between the operating parameters and the three announced induced effects. |
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AbstractList | This paper presents a numerical simulation of the laser shock peening (LSP) process using the finite element method. The majority of controlling parameters of the LSP process have been taken into account. The LSP loading has been characterized by the use of a repetitive time Gaussian increment pressure applied uniformly at a circular impacted zone. The utilized model of the treated material behaviour law is the Johnson-Cook’s visco-elastic-plastic coupled with damage. The proposed model leads to determine the LSP surface modifications: (i) the in-depth residual stresses, (ii) the induced plastic strains and (iii) the superficial damage. These modifications can be significantly induced in few cases, particularly when the operating conditions are not well optimized. An application is carried out on the laser peened titanium aero-engine super alloy Ti-6Al-4V. A satisfactory correlation between the computed and experimental results is observed. Also, it is noted that the computed superficial damage values increase with the growth of the maximal peak pressure of the laser spot, which are physically consistent. Otherwise, in order to optimize the laser peening operating conditions, a design of experiments is established. It allows having surface-response relationships between the operating parameters and the three announced induced effects. |
Author | Ayeb, M. Fathallah, R. Seddik, R. Frija, M. Sidhom, H. |
Author_xml | – sequence: 1 givenname: M. surname: Frija fullname: Frija, M. organization: Institute of Applied Sciences and Technology of Sousse (ISSATSo), University of Sousse – sequence: 2 givenname: M. surname: Ayeb fullname: Ayeb, M. email: ayeb.manel2705@gmail.com organization: National Engineering School of Sousse (ENISo), University of Sousse – sequence: 3 givenname: R. surname: Seddik fullname: Seddik, R. organization: National Engineering School of Sousse (ENISo), University of Sousse – sequence: 4 givenname: R. surname: Fathallah fullname: Fathallah, R. organization: National Engineering School of Sousse (ENISo), University of Sousse – sequence: 5 givenname: H. surname: Sidhom fullname: Sidhom, H. organization: National Higher Engineering School of Tunis (ENSIT), University of Tunis |
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Cites_doi | 10.1108/17579861111108572 10.1179/026708409X12490360425846 10.2351/1.521861 10.1016/j.jmatprotec.2007.11.147 10.1117/12.954969 10.1108/17579861111135923 10.1361/105994900770346259 10.1115/1.1645878 10.1016/j.apsusc.2014.02.128 10.1361/105994903770342944 10.1016/S0142-1123(02)00022-1 10.1007/s11665-016-2158-5 10.1115/1.1445149 10.1016/j.ijfatigue.2014.05.015 10.1016/S1006-7191(08)60029-0 10.1016/S0921-5093(99)00698-X 10.4028/www.scientific.net/SSP.216.210 10.1108/17579861111108644 10.1016/j.triboint.2009.04.005 10.1016/S0142-1123(99)00035-3 10.1088/0965-0393/17/1/015010 10.1016/j.msea.2010.10.020 10.1016/S1003-6326(14)63449-X 10.1016/j.ijfatigue.2007.01.033 10.1016/S0924-0136(02)01122-6 10.1007/s12206-012-1263-0 10.1051/epjap:2003037 10.1016/j.apsusc.2015.05.098 10.1016/j.surfcoat.2009.04.029 10.1016/j.surfcoat.2006.02.018 10.1016/j.msea.2012.09.009 10.1201/9781439823620 10.1016/j.matdes.2015.10.022 10.1016/j.ijmachtools.2007.08.021 |
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Copyright | Springer-Verlag London Ltd., part of Springer Nature 2018 Copyright Springer Science & Business Media 2018 The International Journal of Advanced Manufacturing Technology is a copyright of Springer, (2018). All Rights Reserved. Springer-Verlag London Ltd., part of Springer Nature 2018. |
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Keywords | Finite element method (FEM) Residual stresses Damage Surface work hardening Design of experiments (DoE) Laser shock peening (LSP) |
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Snippet | This paper presents a numerical simulation of the laser shock peening (LSP) process using the finite element method. The majority of controlling parameters of... |
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SubjectTerms | CAE) and Design Computation Computer simulation Computer-Aided Engineering (CAD Damage Design of experiments Engineering Finite element method Industrial and Production Engineering Laser shock processing Lasers Mathematical models Mechanical Engineering Media Management Optimization Original Article Peak pressure Peening Process parameters Residual stress Superalloys Titanium base alloys Viscoelasticity |
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Title | Optimization of peened-surface laser shock conditions by method of finite element and technique of design of experiments |
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